AD 98-20-13
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 B2-1A | Airworthiness Directives; Airbus Model A300 Series Airplanes |
| aircraft | Airbus | A300 B2-1C | Airworthiness Directives; Airbus Model A300 Series Airplanes |
| aircraft | Airbus | A300 B2-203 | Airworthiness Directives; Airbus Model A300 Series Airplanes |
| aircraft | Airbus | A300 B2K-3C | Airworthiness Directives; Airbus Model A300 Series Airplanes |
| aircraft | Airbus | A300 B4-103 | Airworthiness Directives; Airbus Model A300 Series Airplanes |
| aircraft | Airbus | A300 B4-203 | Airworthiness Directives; Airbus Model A300 Series Airplanes |
| aircraft | Airbus | A300 B4-2C | Airworthiness Directives; Airbus Model A300 Series Airplanes |
Unsafe Condition
Corrosion on the fuselage skin panels that surround the emergency exits immediately aft of the wing could result in reduced structural integrity of the fuselage pressure vessel.
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Required Actions
Perform a visual inspection to detect corrosion on the fuselage skin panels between frames 55 to 58 and stringers 13 to 31, left and right, in accordance with Airbus Service Bulletin A300-53-301. If corrosion is found, rework and measure residual thickness; repair with a doubler or replace affected areas if measurements exceed limits. Repeat inspections every 18 months unless repaired.
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Compliance Time
Within 18 months after the effective date of this AD (October 27, 1998).
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Affected Aircraft
Airbus Model A300 series airplanes listed in Airbus Service Bulletin A300-53-301, Revision 1, dated February 20, 1997, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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